Obiekt

Tytuł odmienny:

Modelowanie i badanie dynamicznych właściwości wyrzutni z niesterowanymi pociskami rakietowymi ; Modelowanie i badanie dynamicznych właściwości wyrzutni z niesterowanymi pociskami rakietowymi

Współtwórca:

Maciej NYCKOWSKI ; Maciej NYCKOWSKI

Abstrakt:

The work analyses the operation of the ZSMU-70 weapon module. The results allowed for the development of several guidelines, aiming to shape the dynamic properties of the WW-4 launcher in order to improve the effectiveness of the ZSMU-70 module. This meant that research was carried out at a military training ground. Unguided NLPR-70 missiles were launched. The launching process was recorded using a Phantom high-speed digital camera. The recorded images were then analysed using TEMA software. Based on the results of empirical research, a physical and mathematical model of the motion was formulated for both the ZSMU-70 module as well as the WW-4 launcher. A computer programme was developed, and the motion of the system was simulated during the launching of the missiles. The results of the theoretical analysis were compared with the analogous results from the empirical research. Having the theoretical model verified, some system parameters were changed, and guidelines were used to improve the effectiveness of the ZSMU-70 weapon module.
; The work analyses the operation of the ZSMU-70 weapon module. The results allowed for the development of several guidelines, aiming to shape the dynamic properties of the WW-4 launcher in order to improve the effectiveness of the ZSMU-70 module. This meant that research was carried out at a military training ground. Unguided NLPR-70 missiles were launched. The launching process was recorded using a Phantom high-speed digital camera. The recorded images were then analysed using TEMA software. Based on the results of empirical research, a physical and mathematical model of the motion was formulated for both the ZSMU-70 module as well as the WW-4 launcher. A computer programme was developed, and the motion of the system was simulated during the launching of the missiles. The results of the theoretical analysis were compared with the analogous results from the empirical research. Having the theoretical model verified, some system parameters were changed, and guidelines were used to improve the effectiveness of the ZSMU-70 weapon module.

Miejsce wydania:

Warszawa
; Warszawa

Wydawca:

Wojskowa Akademia Techniczna ; Wojskowa Akademia Techniczna

Data utworzenia:

2010 r.0 ; 2010 r.0

Data złożenia:

2022-07-15 ; 2022-07-15

Data akceptacji:

2022-12-12 ; 2022-12-12

Data wydania:

2022-12-30 ; 2022-12-30

Rozmiar:

B5 ; B5

Identyfikator:

oai:ribes-88.man.poznan.pl:2655

Sygnatura:

DOI 10.5604/01.3001.0016.1457 ; DOI 10.5604/01.3001.0016.1457

ISSN elektroniczny:

2720-5266 ; 2720-5266

ISSN drukowany:

2081-5891 ; 2081-5891

Język:

angielski ; angielski

Licencja:

kliknij tutaj, żeby przejść ; kliknij tutaj, żeby przejść

Właściciel praw:

Wojskowa Akademia Techniczna ; Wojskowa Akademia Techniczna

Strona początkowa:

51 ; 51

Strona końcowa:

66 ; 66

Tom:

13 ; 13

Słowa kluczowe:

mechanical engineering, launcher, missiles, empirical research, theoretical analysis ; mechanical engineering, launcher, missiles, empirical research, theoretical analysis